Douglas DC-9-14

Service difficulty reports · 1,736

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC914'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ABXA010773Fitting · crackedLEFT OVER WING EXIT DOOR PAN STIFFENER ANGLES ON OUTER PAN CRACKED 5 INCHES. REPLACED STOPS IAW DC-9 SRM 51-30-2 AND 51-30-5.Feb 27, 2002 · N925AX · Doug DC914 · Emergency ExitsSDR ABXA010772Angle · crackedOUTBOARD LOWER FASTENER HOLE ON ATTACH ANGLE CRACKED WHERE WING TO FUSELAGE FAIRING ATTACHES AT F.S. 585. REPLACED ANGLE IAW DC-9 SRM 51-30-1 AND DC-9 DWG 9915547.Feb 26, 2002 · N925AX · Doug DC914 · Standard Practices/StructuresSDR 0200599154Duct · damagedDURING CLIMBOUT, THE RIGHT ENGINE EXPERIENCED A FIRE WARNING INDICATION. CREW REDUCED RIGHT ENGINE THRUST TO IDLE SETTING AND LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE FUEL HEAT AFeb 26, 2002 · N8913E · Doug DC914 · Air Intake Anti/De-Ice SystemSDR ABXA010771Finger Doubler · debondedOUTBOARD REMOVABLE TRAILING EDGE LOWER SKIN FINGER DOUBLERS WERE DEBONDED. REPLACED UPPER/LOWER SKINS IAW REA D957-43379.Feb 25, 2002 · N925AX · Doug DC914 · Wing, Plate/SkinSDR ABXA010676Control Cable · lack of lubeFINAL APPROACH, AIRCRAFT IN A TRIMMED DESCENT ON GLIDESLOPE, FLAPS 30, N1-60 PERCENT ON BOTH ENGINES, SPEED 10 + OVER TARGET 139. WENT TO FLAP 40, AIRCRAFT ROLLED RIGHT NOTICEABLE, 1 1/2 UNITS LEFT TO TRIM. INSPECTED AILERON AND FLAP CABLE SYSTEM. ALSO INSPJan 16, 2002 · N925AX · Doug DC914 · Trailing Edge Flap Control SystemSDR MWEA020045Spar · crackedRIGHT HAND ELEVATOR FORWARD SPAR HAS A CRACK INDICATION VIEWED ON RADIOGRAPH "RG" AT APPROXIMATELY STATION XE 105 UPPER CAP LOWER SURFACE -- FABRICATED AND HEAT TREAT PARTS. INSTALLED REPAIR SPAR. REBALANCED RIGHT HAND ELEVATOR.Jan 8, 2002 · N500ME · Doug DC914 · Elevator Control SystemSDR MWEA020044Spar · crackedLEFT HAND ELEVATOR FORWARD SPAR HAS A CRACK INDICATION VIEWED ON RADIOGRAPH "LM" AT APPROXIMATELY STATION XE 203 -- LOCATED ENDS OF CRACK. FABRICATED AND INSTALLED REPAIR SPAR. REBALANCED LEFT HAND ELEVATOR.Jan 8, 2002 · N500ME · Doug DC914 · Elevator Control SystemSDR MWEA020043Spar · crackedLEFT HAND ELEVATOR FORWARD SPAR HAS CRACK INDICATION VIEWED ON RADIOGRAPH "LK" AT APPROXIMATELY STATION XE 169 -- LOCATED AND MARKED ENDS OF CRACK. INSTALLED REPAIR SPAR. REBALANCED LEFT HAND ELEVATOR.Jan 8, 2002 · N500ME · Doug DC914 · Elevator Control SystemSDR MWEA011491Switch · faultyAIRCRAFT DEPRESSURIZED DURING CLIMB. REPLACED RIGHT HAND SECOND SEGMENT CLIMB SWITCH.Dec 22, 2001 · N800ME · Doug DC914 · Cabin Pressure Control SystemSDR 0104829156Skin · crackedDuring HCK in DHN, two cracks were discovered per REF. B in the upper fuselage nose skin at stations 76.5 LBL20 & 81 LBL 14.5. At station 76.5, one crack location extended outboard of the trimout of an existing repair. Repaired per EA 91-187461.Dec 10, 2001 · N8915E · Doug DC914 · Fuselage Main, Plate/SkinSDR MWEA011462Door · unsecureNOSE GEAR VIBRATION AFTER GEAR SELECTED UP. RESECURED RIGHT HAND NOSE LANDING GEAR DOOR.Nov 28, 2001 · N600ME · Doug DC914 · Landing Gear DoorsSDR 0104819155Pan · crackedDuring HCK, the forward cargo door inner pan was found to be cracked between stops #1 and #2. The outer pan was also found cracked. Material .050" 2024-t4. Repaired per EA 91-186760.Nov 27, 2001 · N8914E · Doug DC914 · Cargo/Baggage DoorsSDR MWEA011425Bungee Cord · brokenON TAKEOFF, AIRCRAFT CABIN WOULD NOT PRESSURIZE. ADJUSTED FORWARD CARGO DOOR SHIMS ON FORWARD HINGE AND ADJUSTED HINGE SPRINGS. INSTALLED NEW BUNGEE ASSEMBLY ON FORWARD DOOR.Nov 8, 2001 · N600ME · Doug DC914 · Cargo/Baggage DoorsSDR MWEA011419Latch · unsecureAFTER TAKE OFF, AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR MANUAL WITH GOOD PACK PRESSURES. REMOVED DEBRIS IN AFT PORTION OF FWD CARGO DOOR. THE AFT LATCH WAS NOT SECURED ON FWD CARGO DOOR.Nov 6, 2001 · N600ME · Doug DC914 · Cargo/Baggage DoorsSDR MWEA011402Latch · out of adjWHEN RETRACTING THE GEAR, RIGHT MAIN LANDING GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH. EXTENDED GEAR FOR LANDING, ALL INDICATIONS NORMAL. -- ADJUSTED LEFT AND RIGHT MAIN LANDING GEAR LATCH MECHANISMS.Oct 17, 2001 · N600ME · Doug DC914 · Landing Gear Position and WarningSDR MWEA011372Floor Support · crackedFORWARD BAG PIT RIGHT HAND TUNNEL AT STATION 484 SUBFLOOR CRACKED. FABRICATED AND INSTALLED DOUBLER.Oct 11, 2001 · N600ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA011370Stiffener · crackedAPB, AFT SIDE, RADIAL STIFFENER NR 16 LT SIDE HAS A CRACK AT STANDOFF ATTACHMENT. FABRICATED AND INSTALLED REPAIR DOUBLERS.Oct 11, 2001 · N600ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA011373Pin · wornTAIL CONE REQUIRED EXCESSIVE FORCE DURING OPERATIONAL CHECK. REROUTED CABLE AND REPLACED WORN GUIDE PINS.Oct 10, 2001 · N600ME · Doug DC914 · Aerodynamic FairingsSDR 0103229150Controller · failedLOSS OF CABIN PRESSURIZATION DURING CRUISE. CABIN CLIMBED TO 10,500 FEET AT FL290 WITH ANTI-ICE ON AND STEADY CRUISE POWER. FLIGHT DIVERTED TO GRB, REQUESTED CFR BECAUSE OF EXPECTED OVERWEIGHT LANDING CONDITION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLASep 9, 2001 · N8908E · Doug DC914 · Cabin Pressure ControllerSDR MWEA011085Computer · malfunctionedWINDSHEAR LIGHT CAME ON WITH AUTO WARNING. FIRST MAINTENANCE DEFERRED, THEN COLLARD CIRCUIT BREAKER, AND REPLACED THE WINDSHEAR COMPUTER.Jul 28, 2001 · N500ME · Doug DC914 · Doppler SystemSDR 0103829151Duct · crackedDuring an aircraft overnight in MSP at gate G7, The electrical compartment exhaust duct outlet, common to the fuselage skin was found with a crack. The crack length is approximately 1.00" and is in the lower transition from the skin contour to the duct exhaustJul 20, 2001 · N8909E · Doug DC914 · Fuselage Main, StructureSDR MWEA011060Servo · inoperativeWITH AUTOPILOT AND ELEVATOR SERVO OFF TRIM MOVES UNCOMMANDED NOSE UP AND NOSE DOWN. -- REPLACED ELEVATOR SERVO, OPERATIONAL CHECK GOOD.Jul 19, 2001 · N800ME · Doug DC914 · Autopilot Main ServoSDR MWEA011059Transceiver · failedRADAR SCREEN DISPLAYS "RT" AND SHOWS NO WEATHER. -- REMOVED AND REPLACED WEATHER RADAR TRANSCEIVER.Jul 19, 2001 · N600ME · Doug DC914 · Independent Position Determining SystemSDR MWEA011057Wire · brokenSTICK SHAKER CAME ON AFTER ROTATION. -- REPAIRED BROKEN WIRE ON RIGHT FLAP POSITION TRANSMITTER.Jul 17, 2001 · N700ME · Doug DC914 · Trailing Flap Position Indicating SystemSDR MWEA011054Skin · crackedNUMEROUS CRACKS ON LEFT WING UPPER AND LOWER INNER SKIN OF #2 LEADING EDGE, BETWEEN STATIONS XFS 202.400 - 299.939. -- REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS.Jul 17, 2001 · N700ME · Doug DC914 · Wing, Attach FittingsSDR MWEA011053Cap · crackedCRACK INDICATION ON LEFT HORIZONTAL STABILIZER REAR SPAR LOWER CAP, EXTENDING BETWEEN TWO RIVETS, CONFIRMED BY HFEC STATION XHS 146 APPROXIMATELY. -- REMOVED CORROSION, FABRICATED FILLER, DRILLED AND INSTALLED REPAIR ANGLE AND FILLER.Jul 17, 2001 · N700ME · Doug DC914 · Horizontal Stabilizer StructureSDR MWEA011052Skin · dentedLEFT WING LEADING EDGE HAS EIGHT DENTS BETWEEN XRS 214-267. REMOVED DAMAGED AREAS, FABRICATED AND LOCATED EXTERNAL DOUBLER, FABRICATED INTERNAL FILLER AND DOUBLER, LOCATED AND DRILLED INTERNAL FILLERS AND DOUBLER, INSTALLED EXTERNAL DOUBLER.Jul 17, 2001 · N700ME · Doug DC914 · Wing, Plate/SkinSDR MWEA011048Cap · cracked3 1/2" CRACK FOUND ON LEFT UPPER FORWARD SPAR CAP 2 1/2" OUTBOARD OF XCW 58.5 AS VIEWED THROUGH ACCESS PANEL. -- TRIMMED OUT CRACK, TRIMMED AND LOCATED FILLERS, NESTED ANGLE, STIFFNER, INSTALLED FILLER AND ANGLE.Jul 16, 2001 · N700ME · Doug DC914 · Wing Main, Frame StructureSDR MWEA011047Frame · corrodedFORWARD CARGO BAY HAS CORROSION ON FRAME 427 AFT SIDE AND BOTTOM, FROM LONGERON 28 LEFT TO 28 RIGHT. -- REMOVED CORROSION, FLOOR SUPPORTS, DAMAGED SECTION OF FRAME, LOCATED NEW FRAME, INSTALLED FRAME SECTION AND DOUBLERS.Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, StructureSDR MWEA011046Intercostal · damagedLOWER AFT CARGO DOOR JAMB HINGE INTERCOSTAL HAS AN ELONGATED HOLE. -- FABRICATED 2 EACH BUSHING PLATES, INSTALLED PLATES.Jul 16, 2001 · N700ME · Doug DC914 · Cargo/Baggage DoorsSDR MWEA011045Longeron · corrodedFORWARD CARGO BAY HAS CORROSION ON LONGERON 29 RIGHT AT STATION 446 TO 465 AROUND RIVETS. -- REMOVED CORROSION, REMOVED DAMAGED SECTION OF LONGERON, LOCATED NEW LONGERON SECTION, LOCATED AND DRILLED NEW SPLICE, INSTALLED NEW LONGERON SECTION AND SPLICE.Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, StructureSDR MWEA011044Frame · corrodedFORWARD CARGO BAY HAS CORROSION ON FRAME 389 AFT SIDE AT LONGERONS 28 LEFT TO 28 RIGHT. -- BLENDED CORROSION, FABRICATED AND LOCATED DOUBLERS, LOCATED NEW FRAME SECTION, INSTALLED FRAME REPAIR SPLICE.Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, StructureSDR MWEA011043Frame · bentFORWARD CARGO BAY DOOR JAMB FRAME IS BENT AT STATION 378 LONGERON 29 LEFT TO 29 RIGHT. -- RE-CONTOURED BEND, FABRICATED AND INSTALLED REPAIR DOUBLER.Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, StructureSDR MWEA011042Pan · crackedFORWARD CARGO DOOR FORWARD UPPER CORNERS ON THE INNER PAN IS CRACKED AROUND A SEAL FASTENER HOLE. -- LOCATED, DRILLED AND INSTALLED NEW PAN.Jul 16, 2001 · N700ME · Doug DC914 · Cargo/Baggage DoorsSDR MWEA011041Longeron · crackedLONGERON 2 LEFT IS CRACKED WHERE IT ATTACHES TO FRAME AT STATION 897. -- REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, LOCATED, DRILLED NEW SECTION OF LONGERON, INSTALLED REPAIR PARTS.Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, StructureSDR MWEA011040Longeron · crackedLONGERON 2 RIGHT IS CRACKED WHERE IT ATTACHES TO FRAME AT STATION 897. -- REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, LOCATED AND DRILLED NEW SECTION OF LONGERON, INSTALLED REPAIR PARTS.Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, StructureSDR MWEA011039Angle · crackedSTATION 897 AT LONGERON 2 RIGHT SUPPORT ANGLE IS CRACKED. -- REMOVED, FABRICATED AND INSTALLED SUPPORT ANGLE.Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, StructureSDR MWEA011038Angle · crackedSTATION 897 CRACKED AT LONGERON 2 LEFT, ALSO SUPPORT ANGLE AT THAT STATION IS CRACKED. -- FABRICATED GUSSET, LOCATED SUPPORT ANGLE, INSTALLED SUPPORT ANGLE.Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, StructureSDR MWEA011037Longeron · damagedTWO MISDRILLED HOLES IN LONGERON 17 RIGHT AT STATION 897. -- FABRICATED AND LOCATED NEW LONGERON SECTION AND SPLICE, INSTALLED NEW LONGERON AND SPLICE.Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, StructureSDR MWEA011036Longeron · crackedSTATION 897 AT LONGERON 2 RIGHT IS CRACKED. -- REMOVED DAMAGE, TRIMMED AND LOCATED SPLICES AND FRAME, INSTALLED REPAIR PARTS.Jul 16, 2001 · N700ME · Doug DC914 · Fuselage Main, StructureSDR MWEA011035Seat Track · wornCAPTAINS AFT OUTBOARD SEAT TRACK IS WORN AROUND LOCK PIN HOLES. -- REMOVED DAMAGE FROM SEAT TRACK UPPER CAP SURFACE, FABRICATED AND INSTALLED REPAIR DOUBLER.Jul 12, 2001 · N700ME · Doug DC914 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA011034Web · dentedFORWARD CARGO BAY DOOR JAMB WEB HAS A SHARP DENT AT STATION 351 LONGERON 29 RIGHT. -- REMOVED DOOR JAMB WEB, LOCATED, DRILLED AND INSTALLED NEW WEB.Jul 12, 2001 · N700ME · Doug DC914 · Cargo/Baggage DoorsSDR MWEA011033Seat Track · wornFIRST OFFICERS OUTBOARD SEAT TRACK IS WORN AROUND LOCK PIN HOLES. -- FABRICATED, LOCATED, DRILLED AND INSTALLED NEW SEAT TRACK.Jul 12, 2001 · N700ME · Doug DC914 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA011032Seat Track · wornCAPTAINS AFT INBOARD SEAT TRACK IS WORN AROUND LOCK PIN HOLES. -- REMOVED DAMAGED FROM SEAT TRACK, FABRICATED AND INSTALLED REPAIR DOUBLER.Jul 12, 2001 · N700ME · Doug DC914 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA011031Seat Track · wornFIRST OFFICERS AFT INBOARD SEAT TRACK IS WORN AROUND LOCK PIN HOLES. -- REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER.Jul 12, 2001 · N700ME · Doug DC914 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA011030Former · tool damageTOOLING MARKS ON FORMER AFT SIDE BETWEEN LONGERON 28 RIGHT AND 27 RIGHT STATION 120. -- BLENDED TOOLING MARKS, REMOVED DAMAGED FORMER, FORMED NEW FORMER, LOCATED FASTENER HOLES, FABRICATED 2 REPAIR SPLICES, INSTALLED FORMER SECTION.Jul 12, 2001 · N700ME · Doug DC914 · Fuselage Main, StructureSDR MWEA011029Frame · corrodedAFT CARGO STATION 786 FRAME HAS LIGHT CORROSION ON AFT SIDE AND UNDER BOTTOM LIP BETWEEN LONGERONS 28 LEFT AND 29 RIGHT. -- REMOVED DAMAGED SECTION OF FRAME, LOCATED AND DRILLED NEW SECTION, FABRICATED NEW INTERCOSTAL SPLICE, INSTALLED FRAME SPLICE DOUBLER AJul 12, 2001 · N700ME · Doug DC914 · Fuselage Main, StructureSDR MWEA011028Longeron · crackedLEFT SIDE LONGERON 17 IS CRACKED AT STATION 801. -- REMOVED DAMAGED SECTION, DRILLED AND INSTALLED NEW SECTION OF LONGERON AND SPLICE.Jul 10, 2001 · N700ME · Doug DC914 · Fuselage Main, StructureSDR MWEA011027Clip · crackedLEFT SIDE SHEAR CLIP ON LONGERON 17 AT STATION 786 IS CRACKED AT THE FASTENER HOLE. -- REMOVED SHEAR CLIP, FABRICATED AND INSTALLED SHEAR CLIP.Jul 10, 2001 · N700ME · Doug DC914 · Fuselage Main, StructureSDR MWEA011026Longeron · corrodedAFT CARGO LONGERON 26 LEFT HAS LIGHT CORROSION ALONG TOP VERTICAL LEG BETWEEN STATION 750-786. -- REMOVED LONGERON SECTION, LOCATED AND INSTALLED NEW LONGERON.Jul 10, 2001 · N700ME · Doug DC914 · Fuselage Main, Structure
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